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01554cam#a22004813a#4500 |
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INGC-MON-10400 |
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AR-LpUFI |
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20221019004008.0 |
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060510s1969 |||a fr||||| |0 0|eng d |
| 080 |
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|a 629.7
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| 100 |
0 |
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|a Little, B. H.
|9 286691
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| 245 |
0 |
0 |
|a Advantages and Problems of large subsonic aircraft
|
| 260 |
|
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|b National Technical Information Service,
|c 1969.
|
| 300 |
|
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|a p. 583
|
| 440 |
0 |
0 |
|a Von Karman Institute for Fluid Dynami
|9 286692
|
| 599 |
|
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|a Ubic.:629.7 VKI PRES
|
| 650 |
1 |
4 |
|a AERODINAMICA
|9 268671
|
| 650 |
1 |
4 |
|a FLUJO TRANSONICO
|9 283670
|
| 650 |
1 |
4 |
|a AVIONES SUBSONICOS
|9 286693
|
| 650 |
1 |
4 |
|a EFECTO DEL TAMAÑO
|9 286694
|
| 650 |
1 |
4 |
|a DIMENSIONES
|9 269423
|
| 650 |
1 |
4 |
|a FLUTTER
|9 274621
|
| 650 |
1 |
4 |
|a INTERFERENCIA AERODINAMICA
|9 283688
|
| 650 |
1 |
4 |
|a AEROELASTICIDAD
|9 274620
|
| 650 |
1 |
4 |
|a ONDAS DE CHOQUE
|9 283779
|
| 650 |
1 |
4 |
|a SEPARACION DEL FLUJO
|9 286695
|
| 650 |
1 |
4 |
|a EFECTOS DE ESCALA
|9 286696
|
| 650 |
1 |
4 |
|a RESISTENCIA AERODINAMICA
|9 283585
|
| 650 |
1 |
4 |
|a RUIDO AERONAUTICO
|9 286697
|
| 650 |
1 |
4 |
|a DISEÑO DE AERONAVES
|9 272447
|
| 650 |
1 |
4 |
|a DISEÑO DE ALAS
|9 275135
|
| 650 |
1 |
4 |
|a DISEÑO DE FUSELAJE
|9 284505
|
| 650 |
1 |
4 |
|a PERFILES SUPERCRITICOS
|9 286698
|
| 650 |
1 |
4 |
|a DISEÑO DE PERFILES
|9 275134
|
| 650 |
1 |
4 |
|a HIPERSUSTENTADORES
|9 283600
|
| 650 |
1 |
4 |
|a DISEÑO DE AERONAVES
|9 272447
|
| 650 |
1 |
4 |
|a DISEÑO POR COMPUTADORA
|9 286699
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| 942 |
|
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|c LIB
|6 _
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| 959 |
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|a MON
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| 960 |
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|a 11112
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| 970 |
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|a Registro convertido en forma automatizada
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| 999 |
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|c 10398
|d 10398
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| 040 |
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|a AR-LpUFI
|c AR-LpUFI
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